Constant amplitude fatigue tests of 72 P-51D "Mustang" wings performed by vibrational loading system and by hydraulic loading device for conditions with and without varying amounts of preload. Originally issued as Report ARL/SM 207, Aeronautical Research Laboratories, Australia.
Interim report on fatigue characteristics of typical metal wing
NACA -- Tech Memo
1956
80 pages
Report
Englisch
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Interim report on fatigue investigation of full-scale transport aircraft wing structure
Engineering Index Backfile | 1953
|Flutter Characteristics of Typical Wing Sections of a Box Wing Aircraft Configuration
BASE | 2018
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